基于深度学习的梯度下降多算法网格搜索优化传感器融合

T. M. Booth, Sudipto Ghosh
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引用次数: 1

摘要

传感器融合方法将来自一套传感器的数据组合成一个集成的解决方案,比单个传感器产生的数据更准确地代表目标环境。基于深度学习(DL)的方法可以比传统方法更准确地解决传感器融合的挑战。然而,当传感器在传感器系统中被修改、升级或交换时,所选方法的准确性可能会发生变化。从历史上看,这可能需要昂贵的手动重构传感器融合解决方案。本文开发了12种基于深度学习的传感器融合方法,并提出了一种系统的迭代方法,用于同时选择最优深度学习方法和超参数设置。梯度下降多算法网格搜索(GD-MAGS)方法是一种迭代网格搜索技术,通过梯度下降预测得到增强,并扩展到跨并发运行的基于dl的方法交换性能测量信息。此外,在每次迭代中,随着超参数调优带来的计算费用增加,将对性能最差的两种深度学习方法进行修剪,以减少资源使用。我们使用一个开源的时间序列飞机数据集来评估这种方法,该数据集是在飞机高度上训练的,使用多模态传感器来测量诸如速度、加速度、压力、温度和飞机方向和位置等变量。我们展示了最佳深度学习模型的选择,与分析的其他11种深度学习方法相比,模型精度提高了88%。对所选模型的验证表明,该模型在使用相同传感器系统的其他飞机上的数据优于裁剪模型。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
A Gradient Descent Multi-Algorithm Grid Search Optimization of Deep Learning for Sensor Fusion
Sensor fusion approaches combine data from a suite of sensors into an integrated solution that represents the target environment more accurately than that produced by an individual sensor. Deep learning (DL) based approaches can address challenges with sensor fusion more accurately than classical approaches. However, the accuracy of the selected approach can change when sensors are modified, upgraded or swapped out within the system of sensors. Historically, this can require an expensive manual refactor of the sensor fusion solution.This paper develops 12 DL-based sensor fusion approaches and proposes a systematic and iterative methodology for selecting an optimal DL approach and hyperparameter settings simultaneously. The Gradient Descent Multi-Algorithm Grid Search (GD-MAGS) methodology is an iterative grid search technique enhanced by gradient descent predictions and expanded to exchange performance measure information across concurrently running DL-based approaches. Additionally, at each iteration, the worst two performing DL approaches are pruned to reduce the resource usage as computational expense increases from hyperparameter tuning. We evaluate this methodology using an open source, time-series aircraft data set trained on the aircraft’s altitude using multi-modal sensors that measure variables such as velocities, accelerations, pressures, temperatures, and aircraft orientation and position. We demonstrate the selection of an optimal DL model and an increase of 88% in model accuracy compared to the other 11 DL approaches analyzed. Verification of the model selected shows that it outperforms pruned models on data from other aircraft with the same system of sensors.
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